Unsteady control surface pressure measurements and computation

A. Karlsson; B. Winzell; P. Eliasson; J. Nordstrom; L. Torngren; L. Tysell

Unsteady control surface pressure measurements and computation

A. Karlsson, B. Winzell, P. Eliasson, J. Nordstrom, L. Torngren, L. Tysell

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution › peer-review

6 Citations (Scopus)

Abstract

Measurements of steady and unsteady pressure due to flap deflection and oscillation will be presented. The test contains a variation in Mach number, excitation frequency, angle of attack, mean flap angle and Reynolds number. Interesting features of flow separation over the control surface are included. Comparison with computations will be done.

Original language	English
Title of host publication	14th Applied Aerodynamics Conference
Publisher	American Institute of Aeronautics and Astronautics Inc, AIAA
Pages	340-348
Number of pages	9
ISBN (Print)	9781563472121
Publication status	Published - 1996
Externally published	Yes
Event	14th Applied Aerodynamics Conference, 1996 - New Orleans, United States Duration: 17 Jun 1996 → 20 Jun 1996

Publication series

Name	14th Applied Aerodynamics Conference

Conference

Conference	14th Applied Aerodynamics Conference, 1996
Country/Territory	United States
City	New Orleans
Period	17/06/96 → 20/06/96

ASJC Scopus subject areas

General Engineering

Cite this

@inproceedings{7567736731264598a89fe42b4818f794,

title = "Unsteady control surface pressure measurements and computation",

abstract = "Measurements of steady and unsteady pressure due to flap deflection and oscillation will be presented. The test contains a variation in Mach number, excitation frequency, angle of attack, mean flap angle and Reynolds number. Interesting features of flow separation over the control surface are included. Comparison with computations will be done.",

author = "A. Karlsson and B. Winzell and P. Eliasson and J. Nordstrom and L. Torngren and L. Tysell",

note = "Publisher Copyright: {\textcopyright} 1996 by the American Institute of Aeronautics and Astronautics, Inc. All rights reserved.; 14th Applied Aerodynamics Conference, 1996 ; Conference date: 17-06-1996 Through 20-06-1996",

year = "1996",

language = "English",

isbn = "9781563472121",

series = "14th Applied Aerodynamics Conference",

publisher = "American Institute of Aeronautics and Astronautics Inc, AIAA",

pages = "340--348",

booktitle = "14th Applied Aerodynamics Conference",

}

Karlsson, A, Winzell, B, Eliasson, P, Nordstrom, J, Torngren, L & Tysell, L 1996, Unsteady control surface pressure measurements and computation. in 14th Applied Aerodynamics Conference., AIAA-96-2417, 14th Applied Aerodynamics Conference, American Institute of Aeronautics and Astronautics Inc, AIAA, pp. 340-348, 14th Applied Aerodynamics Conference, 1996, New Orleans, United States, 17/06/96.

Unsteady control surface pressure measurements and computation. / Karlsson, A.; Winzell, B.; Eliasson, P. et al.
14th Applied Aerodynamics Conference. American Institute of Aeronautics and Astronautics Inc, AIAA, 1996. p. 340-348 AIAA-96-2417 (14th Applied Aerodynamics Conference).

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution › peer-review

TY - GEN

T1 - Unsteady control surface pressure measurements and computation

AU - Karlsson, A.

AU - Winzell, B.

AU - Eliasson, P.

AU - Nordstrom, J.

AU - Torngren, L.

AU - Tysell, L.

PY - 1996

Y1 - 1996

N2 - Measurements of steady and unsteady pressure due to flap deflection and oscillation will be presented. The test contains a variation in Mach number, excitation frequency, angle of attack, mean flap angle and Reynolds number. Interesting features of flow separation over the control surface are included. Comparison with computations will be done.

AB - Measurements of steady and unsteady pressure due to flap deflection and oscillation will be presented. The test contains a variation in Mach number, excitation frequency, angle of attack, mean flap angle and Reynolds number. Interesting features of flow separation over the control surface are included. Comparison with computations will be done.

UR - http://www.scopus.com/inward/record.url?scp=84964270620&partnerID=8YFLogxK

M3 - Conference contribution

AN - SCOPUS:84964270620

SN - 9781563472121

T3 - 14th Applied Aerodynamics Conference

SP - 340

EP - 348

BT - 14th Applied Aerodynamics Conference

PB - American Institute of Aeronautics and Astronautics Inc, AIAA

T2 - 14th Applied Aerodynamics Conference, 1996

Y2 - 17 June 1996 through 20 June 1996

ER -

Unsteady control surface pressure measurements and computation

Abstract

Publication series

Conference

ASJC Scopus subject areas

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